000 00670pam a2200205a 44500
003 OSt
005 20220901160909.0
008 220901b xxu||||| |||| 00| 0 eng d
040 _cIIT Kanpur
041 _aeng
100 _aBoldman,Donald R.
245 1 _aPREDICTION OF LOCAL AND INTEGRATED HEAT TRANSFER IN NOZZLES USING AN INTEGRAL TURBULENT BOUNDARY LAYER METHOD
_cDonald R.Boldman and James F. Schmidt
260 _bNASA, Washington, D.C.
_c1972
300 _a28p
440 _aNASA Technical Note
500 _aTechnical Reports D-6590-96 Bound Vol. No.101254; contents: TR9345-53
650 _aAerospace
700 _aSchmidt,James F.
942 _cTR
999 _c393849
_d393849